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4084183 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4084183: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN, overall_height: 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN, overall_length: 2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14; 4.615-4.639 SQ.

IN AREA; DCN 97-13 EC96NA072. This part is cataloged in the U.S. Government catalog under NSN 2840-01-445-5768, indicating validated use in U.S.

government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
4084183
NSN: 2840-01-445-5768
NIINs: 014455768, 014455770, 014455773, 014455775
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialNICKEL ALLOY OVERALL
design_typeAXIAL COMPRESSOR
stage_number3
overall_width2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
overall_height4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN
overall_length2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN
special_featuresT.O. 2J-F100-14; 4.615-4.639 SQ. IN AREA; DCN 97-13 EC96NA072
end_item_identificationF100-PW-100 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationTURBINE
criticality_code_justificationABHP AND ABKW AND ABMK AND FEAT
part_name_assigned_by_controlling_agencyORIGINAL NAME VANE, TURBINE STATOR
NSN2840-01-445-5768
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 4084183 MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: ABHP AND ABKW AND ABMK AND FEAT
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
OVERALL HEIGHT4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN
STAGE NUMBER3
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONABHP AND ABKW AND ABMK AND FEAT
OVERALL LENGTH2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN
OVERALL WIDTH2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATUREST.O. 2J-F100-14; 4.615-4.639 SQ. IN AREA; DCN 97-13 EC96NA072
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME VANE, TURBINE STATOR
END ITEM IDENTIFICATIONF100-PW-100 AIRCRAFT GAS TURBINE ENGINE
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 4084183?
4084183 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What is the NSN for 4084183?
4084183 is cataloged in the U.S. Government catalog under NSN 2840-01-445-5768. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.